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DTG Integrated Navigation System/

Dynamically Tuned Inertial Navigation System

ER-1 (0.4~0.5°):

◆Strapdown inertial navigation system determination of aircraft position, heading, altitude;

◆System with emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding, non volatile storage.

  • Introduction

Dynamically Tuned Inertial Navigation System consists of inertial measurement unit, magnetic heading sensor and control the display, satellite receiving antenna, doppler radar and installation bracket component. The satellite receiving antenna can customized according to the needs for BD2/GPS/GLONASS triple receiving antenna or BD2 anti-interference antenna. Inertial measurement unit can also be a separate form of inertial measurement unit, for all kinds of missile flight control system and guidance system

Strapdown inertial navigation system determines aircraft position, heading, altitude, the acceleration. As the navigation of aircraft, it determines flight control, route management and provides location, velocity, attitude, heading information. Dynamically Tuned Inertial Navigation System has emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding and non volatile storage.

  • Specifications
    Project ER-1[1] ER-1A[2] ER-1N[3]
    Overall Dimensions 1/2ATRStandard Case315mm×124mm×194mm 1/2ATRStandard Case315mm×124mm×194mm 1/2ATRStandard Case315mm×124mm×194mm
    Weight ≤12kg ≤22.33kg (Containing Doppler radar) ≤8.5kg
    Power Supply 28V DC Power Consumption≤90W 28V DC Power Consumption≤65W 28V DC Power Consumption≤60W
    Preparation Time (Starting At Normal Temperature) Normal Condition8minEmergency Situation2min Normal Condition8minEmergency Situation3min Normal Condition6minEmergency Situation3min
    Precision Of Integrated Navigation Position: 30m(CEP)Speed: 1m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 30m(CEP)Speed: 1m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 30m(CEP)Speed: 0.5m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS)
    Pure Inertia Navigation Accuracy Position: 10km/30min(CEP)Speed: 6m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 10km/20min(CEP)Speed: 5m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 1.5nm/10min(CEP)Speed: 6m/s(RMS) Heading: 0.5°(RMS) Attitude: 0.2°(RMS)
    Inertial / Doppler Integrated Navigation Accuracy Position: 1%·S,S For The Flying DistanceSpeed: Not Less Than Doppler Radar Accuracy Heading: 0.4°(1σ) Attitude: 0.2°(1σ) Position: 0.8%·S,S For The Flying DistanceSpeed: Not less Than Doppler Radar Accuracy Heading: 0.5°(1σ) Attitude: 0.2°(1σ)
    Precision Of Satellite Navigation Position: 30m(CEP)Speed: 1m/s(RMS) Position:30m(CEP)Speed: 1m/s(RMS) Position:30m(CEP)Speed: 0.8m/s(RMS)
    Dynamic Adaptability Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥200°/S2 Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥200°/S2 Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥300°/S2
    Working Temperature -40ºC~+70℃ -40ºC~+65℃ -40ºC~+60℃
    Storage Temperature -55ºC~+70℃ -55ºC~+70℃ -55ºC~+70℃
    Vibration 0.0027g2/HZ 0.02g2/HZ 0.02g2/HZ
    Shock 15g 15g 15g

    Note[1]: contains the control display.

    Note[2]: contains Doppler radar.

    Note[3]: with moving base alignment and DVS current correction function.

  • FAQ

    1. What are the quotation methods?

    If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.

    2. Are there any discounts?

    After we submit the sample price, if more quantity is needed, we will quote the bulk price.

    3. How long will it take to deliver the goods after placing the order?

    For sensors, parts and modules: in stock-one week; no stock-2-4weeks; For systems, generally, 8-12 weeks.

    4. How to deal with the quality problems?

    After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.

    If interested in Dynamically Tuned Inertial Navigation System, pls contact us : [email protected]

  • Project ER-1[1] ER-1A[2] ER-1N[3]
    Overall Dimensions 1/2ATRStandard Case315mm×124mm×194mm 1/2ATRStandard Case315mm×124mm×194mm 1/2ATRStandard Case315mm×124mm×194mm
    Weight ≤12kg ≤22.33kg (Containing Doppler radar) ≤8.5kg
    Power Supply 28V DC Power Consumption≤90W 28V DC Power Consumption≤65W 28V DC Power Consumption≤60W
    Preparation Time (Starting At Normal Temperature) Normal Condition8minEmergency Situation2min Normal Condition8minEmergency Situation3min Normal Condition6minEmergency Situation3min
    Precision Of Integrated Navigation Position: 30m(CEP)Speed: 1m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 30m(CEP)Speed: 1m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 30m(CEP)Speed: 0.5m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS)
    Pure Inertia Navigation Accuracy Position: 10km/30min(CEP)Speed: 6m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 10km/20min(CEP)Speed: 5m/s(RMS) Heading: 0.4°(RMS) Attitude: 0.2°(RMS) Position: 1.5nm/10min(CEP)Speed: 6m/s(RMS) Heading: 0.5°(RMS) Attitude: 0.2°(RMS)
    Inertial / Doppler Integrated Navigation Accuracy Position: 1%·S,S For The Flying DistanceSpeed: Not Less Than Doppler Radar Accuracy Heading: 0.4°(1σ) Attitude: 0.2°(1σ) Position: 0.8%·S,S For The Flying DistanceSpeed: Not less Than Doppler Radar Accuracy Heading: 0.5°(1σ) Attitude: 0.2°(1σ)
    Precision Of Satellite Navigation Position: 30m(CEP)Speed: 1m/s(RMS) Position:30m(CEP)Speed: 1m/s(RMS) Position:30m(CEP)Speed: 0.8m/s(RMS)
    Dynamic Adaptability Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥200°/S2 Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥200°/S2 Angular Velocity≥±100°/SLinear Acceleration≥±8g Angular Acceleration≥300°/S2
    Working Temperature -40ºC~+70℃ -40ºC~+65℃ -40ºC~+60℃
    Storage Temperature -55ºC~+70℃ -55ºC~+70℃ -55ºC~+70℃
    Vibration 0.0027g2/HZ 0.02g2/HZ 0.02g2/HZ
    Shock 15g 15g 15g

    Note[1]: contains the control display.

    Note[2]: contains Doppler radar.

    Note[3]: with moving base alignment and DVS current correction function.

    1. What are the quotation methods?

    If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.

    2. Are there any discounts?

    After we submit the sample price, if more quantity is needed, we will quote the bulk price.

    3. How long will it take to deliver the goods after placing the order?

    For sensors, parts and modules: in stock-one week; no stock-2-4weeks; For systems, generally, 8-12 weeks.

    4. How to deal with the quality problems?

    After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.

    If interested in Dynamically Tuned Inertial Navigation System, pls contact us : [email protected]